JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5730' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5730' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AMW060705011ASkin · bird strikeBIRD STRIKE DAMAGE TO LT WING CENTER LEADING EDGE. DAMAGE 6IN X 3IN X 1IN DEEP. DAMAGE REPAIRED IAW AIR MIDWEST TO 1900-57-20-0006.SDR UPS06247455Panel · delaminatedINSPECTION TYPE:C LT WING UPPER SURFACE PANEL FWD OF NR 5 AND 6 SPOILERS DELAM AT PREVIOUS REPAIR. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-40-20. PANEL REPLACED IAW SRM 51-30-02.SDR QXEA200601832Panel · corrodedPDX C4 - RIGHT HAND FUEL PANEL 624CT HAS PITTING CORROSION ON COUNTER SINK HOLES. REPLACED PANEL WITH SERVICEABLE FROM STOCK.SDR QXEA200601783Access Panel · corrodedPDX C4 - LEFT FUEL PANEL 524BT HAS LIGHT PITTING CORROSION IN COUNTER SINK HOLES. REFERENCE PANEL CARD P22 FOR INSTALLATION OF SERVICEABLE PANEL.SDR QXEA200601782Access Panel · corrodedPDX C4 - LEFT FUEL PANEL 524BT HAS LIGHT SURFACE CORROSION AROUND SCREW HOLES. REFERENCE PANEL CARD P22 FOR INSTALLATION OF SERVICEABLE PANEL.SDR QXEA200601781Access Panel · corrodedPDX C4 - FOUND LEFT FUEL PANEL NR 524AT HAS LIGHT PITTING CORROSION IN COUNTER SINK HOLES. REFERENCE PANEL CAR P22 FOR INSTALLATION.SDR QXEA200601780Access Panel · corrodedPDX C4 - LEFT FUEL PANEL NR 524CT HAS PITTING CORROSION IN COUNTER SINK HOLES. REFERENCE PANEL CARD P22 FOR INSTALLATION OF SERVICEABLE PANEL.SDR QXEA200601779Access Panel · corrodedPDX C4 - LEFT FUEL PANEL NR 524CT HAS LIGHT SURFACE CORROSION AROUND SCREW HOLES. REFERENCE PANEL CARD P22 FOR INSTALLATION OF SERVICEABLE PANEL.SDR QXEA200601778Access Panel · corrodedPDX C4 - LEFT FUEL PANEL NR 524CT HAS PITTING CORROSION IN COUNTER SINK HOLES. REFERENCE PANEL CARD P22 FOR INSTALLATION OF SERVICEABLE PANEL.SDR QXEA200601777Access Panel · corrodedPDX C4 - RIGHT FUEL PANEL NR 624CT HAS SURFACE CORROSION AROUND SCREW HOLES OF PANEL. REPLACED PANEL CARD P19 FOR INSTALLATION OF SERVICEABLE PANEL.SDR CALA0600237Skin · corrodedINSPECTION FOUND CORROSION ON AFT INTERIOR SURFACE OF THE LT WING AFT FUEL BOOST PUMP SKIN CUTOUT AT WS 70.85-140. A REPAIR WAS INSTALLED IAW ECRA 5720-01990.SDR IXXA06SMN198SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E UPPER SKIN CORRODED BETWEEN XW 257.000 AND XW 261.000.SDR IXXA06SMN197SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING.- INBD L/E UPPER SKIN CORRODED BETWEEN XFS 207.000 AND XFS 211.000.SDR IXXA06SMN196SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT WING.- INBD L/E UPPER SKIN CRACKED 2" APPROX BETWEEN XFS 204.000 AND XFS 207.000.SDR IXXA06SMN209SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND WING FLAP PANEL UPPER SKIN DENTED AT STATION XF 364.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 5794 DATED 10-01-02. REMOVED DAMAGED PANEL SKIN IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21.SDR THMN4165SQ118Skin · crackedCRACK IN RT WING OB SKIN NEAR SPAR. MADE AIRWORTHY REPAIR IAW PA-39 SERVICE MANUAL CHAPTER 4 PG 1F6 AND AC43.13-1B SECTION 4 PARAGRAPH 4-57 FIGURE 4-6 AND SECTION 4 PARAGRAPH 4-58 FIGURE 4-16SDR UPS06847597Skin · crackedINSPECTION TYPE:C1 LT UPPER WING SKIN CRACKED 1/2" LONG AT STA XCW 69.5 REAR SPAR UPPER SKIN. FABRICATED AND INSTALLED REPAIR -3 FILLER AND -5/-7 DOUBLERS LT UPPER WING SKIN AT XCW 69.5 IAW SRM 57-02-01-0, SAA EA 008-5710- A0314 DTD 2 AUG2006 AND UPS EO DC8 5SDR DHL2006762507Skin · crackedREF NR 072657 DISCREPANCY, RT WING T/E UPPER SURFACE AT NR 13 SPOILER CTR HINGE HAS SKIN CRACKED. REMOVED FASTENERS ON RT T/E UPPER NR 13 SPOILER IAW SRM 51-30-2, CUT OUT DAMAGE SECTION .7500 INCH X ,2500 AT RT WING T/E UPPER SURFACE NR 13 SPOILER HINGE SKIN SDR UIEA2006149Panel · delaminatedL/W-L/E PANEL DELAMINATION UPPER SURFACE APPROX 14"BY 26". PANEL BEHIND NR 9 L/E DEVICE. REMOVED DAMAGED AREA, SANDED AND CLEANED AREA AS REQUIRED. PERFORMED HOT BOND REPAIR ON AREA AS PER SRM 51-40-12 NEED TO BE POTTED, PRIME AND PAINTED. POTTED AREA AND SDR UIEA200600148Panel · crackedL/W UPPER L/E PANEL CRACKED LENGTHWISE APPROX 44". PANEL IS BEHIND NR 2 PYLON. REMOVED DAMAGED AREA, SANDED AND CLEANED AREA AS REQUIRED. PERFORMED HOT BOND REPAIR ON AREA AS PER SRM 51-40-12 NEEDS TO BE POTTED PRIMED AND PAINTED. POTTED AREA AND CURING PESDR 06FDEA2433Skin Panel · crackedRIGHT HAND WING - 3EA FASTENER HOLES FOUND CRACKED ON ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6, STRINGER 36, LOWER SKIN PANEL. COMPLIED WITH FEDEX E.A. #1-5710-100665, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2432Skin Panel · crackedSNRM N00955: LEFT HAND WING - 3EA FASTENER HOLES FOUND CRACKED ON ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713-6, STRINGER 36, LOWER SKIN PANEL. COMPLIED WITH FEDEX E.A. #1-5710-100663SDR QXEA200602233Skin Panel · unknownPDX: RT CENTER WING FUEL PANEL 622AT, 622BT, 622CT AND 623AT REBATES TOP SURFACE REQUIRES STRIPPING AND CLEANING FOR DVI AND ANCHOR NUT GANG CHANNELS REQUIRE REMOVAL FOR ACCESS. MAINTENANCE REPAIRED IAW Q400 SRM 51-26-10-150-801, SRM 51-26-00-110-801, SRM 51-SDR QXEA200602232Panel · damagedPDX: LT CENTER WING FUEL PANEL 522AT, 522BT, 522CT AND 523AT REBATES TOP SURFACE REQUIRES STRIPPING AND CLEANING FOR DVI AND ANCHOR NUT GANG CHANNELS REQUIRE REMOVAL FOR ACCESS. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05-330-801, SRM 51-40-15-330-801, SRM 51-SDR DHL2006762523Skin Panel · delaminatedL/WING TE UPPER PANEL DELAMINATED AT LWBL 88 BS 889 IN/SQ WITH NO CRACKS EVIDENT IN OUTER SKIN. CUT OUT DELAMINATED AREA ON UPPER SKIN OF L/WING TE PANEL APPROX 10" DIA. FABRICATED DOUBLER 14" DIA FROM .016" 7075T6 PO# 526029 AND BONDED. REMOVED SECTION OF SDR MWEA060100Doubler · crackedLEFT WING, LEADING EDGE CAVITY HAS A CRACK IN THE INTERNAL DOUBLER AT THE PRODUCTION BUTT JOINT, LOCATED AT WING STATION XFS 194.850. -- FABRICATED AND INSTALLED FILLER & STRAP.SDR MWEA060099Skin · corrodedCORROSION IN RIGHT WING LOWER SKIN JUST OUTBOARD OF FUELING VALVE & CONTROL PANEL. FABRICATED AND INSTALLED DOUBLER.SDR TRAX200600425Skin · corrodedSOME WING FUEL TANK ACCESS OPENINGS HAVE PITTING CORROSION. (MARKED)SDR I5W2006F00000Skin Panel · corrodedTHIS AIRCRAFT WENT INTO MAINT ON 4/20/2006 FOR REPLACEMENT OF THE LEFT WING DEICE BOOT. SEVERE CORROSION WAS NOTED ON LOWER WING SKIN PANEL, PN 652200497, WHEN BOOT WAS REMOVED. PANEL REQUIRED REPLACEMENT. SL, WINGS-NOTIFICATION OF LEADING EDGE SKIN REWORK SDR IXXA06SMN184SPanel · crackedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS, STA XFS 194.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN183SPanel · crackedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS, STA XFS 194.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN182SPanel · crackedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS, STA XFS 80.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN195SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, NR 1 LT STUB WING UPPER SKIN CORRODED ON SOME AREAS, STA XFS 554.000.SDR IXXA06SMN194SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD L/E OUTER SECTION UPPER SKIN CORRODED ON SOME AREAS, STA XFS 803.000.SDR IXXA06SMN193SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, NR 1 LT STUB WING UPPER SKIN CORRODED ON SOME AREAS, STA XFS 530.000.SDR IXXA06SMN192SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD L/E OUTER SECTION UPPER SKIN CORRODED ON SOME AREAS , STA XFS 747.000.SDR 2006FA0000607Skin · crackedDURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE LT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEARESDR 2006FA0000606Skin · crackedDURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE LT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEARESDR 2006FA0000622Skin · crackedDURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE RT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEARESDR 2006FA0000621Skin · crackedDURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE RT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEARESDR QXEA200601896Panel · corrodedPDX C3 - RIGHT WING STRESS PANEL 622CT MATING SURFACE AROUND FASTENER HOLES HAS PITTING CORROSION. REPAIRED IAW RD 8/4-57-688 AND HORIZON AIR EO 6-57-505.SDR QXEA200601889Panel · corrodedPDX C3 - RIGHT WING STRESS PANEL NR 622BT MATING SURFACE AROUND FASTENER HOLES HAS PITTING CORROSION. REPAIRED IAW RD 8/4-57-441.SDR UIEA200600163Skin · corrodedUPON REMOVAL OF TAPER LOCK FASTENER AT WS1084 FOUND WING INNERSPAR LOWER SKIN PADDED AREA WITH CORROSION BETWEEN FSSI 1111-1114. REMOVED CORROSION AND CARRIED OUT REPAIR ON RIGHT WING ILES 1116.0 LOWER SKIN PADDED AREA PER BOEING RESPONSE MSG NR 1-201142367-5SDR QXEA200601903Panel · corrodedPDX C3 - RIGHT WING STRESS PANEL 622AT MATING SURFACE AROUND FASTENER HOLES HAS PITTING CORROSION. REPAIRED IAW RD 8/4-57-0441.SDR A6WA200640263Skin · corrodedTHE LEFT LOWER WING PLANK HAS MINOR CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 540DB HOLE NR 6 AT WS 95.950 APPROX .003 DEEP BY .4 INCH LONG ON THE FORWARD HOLE EDGE AND .003 DEEP BY .4 INCH LONG ON THE AFT HOLE EDGE IN THE CRITICAL AREAS. MAINTENANCESDR A6WA200640260Skin · corrodedTHE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550FB HOLE NR 14 AT WS 274.319 APPROX .005 INCH DEEP BY 1.5 INCH LONG ON THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .005 INCH BY .75 INCH IN THE CRITICAL AREA ON THE AFSDR A6WA200640259Skin · corrodedTHE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550EB HOLE NR 13 AT WS 253.022 APPROX .004 INCH DEEP BY 1 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .004 INCH DEEP BY .75 INCH LONG IN THE CRITICAL AREA OSDR A6WA200640258Skin · corrodedTHE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550DB HOLE NR 12 AT WS 230.415 APPROX .004 INCH DEEP BY 1.25 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .004 INCH DEEP BY .75 INCH LONG IN THE CRITICAL ARESDR A6WA200640257Skin · corrodedTHE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550BB HOLE NR 10 AT WS 188.040 APPROX .005 INCH DEEP BY 2.75 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .005 INCH DEEP BY 1.25 INCH LONG IN THE CRITICAL ARSDR A6WA200640256Skin · corrodedTHE LEFT LOWER WING PLANK HAS CORROSION AT THE FUEL TANK ACCESS CUTOUT FOR PANEL 550AB HOLE NR 9 WS 163 APPROX .005 INCH DEEP BY .25 INCH LONG IN THE CRITICAL AREA ON THE FORWARD HOLE EDGE AND APPROX .005 INCH BY 1 INCH THE CRITICAL AREA ON THE AFT HOLE EDGE.
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